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Spacecraft reliability/maintainability optimization.Description of a procedure to develop a methodology to optimize man-serviced systems for reliability and maintainability. The spacecraft systems are analyzed using failure modes and effects analysis and maintenance analysis, component mean-time-between failure, duty cycle, type of redundancy, and cost information to develop parametric data on various time intervals. Included are crew time-to-repair, cost, weight, and volume effects of increasing subsystem reliability above the baseline. Results are presented for space systems using the existing data from a research and applications module. These results show the minimum cost of sustaining mission operations.
Document ID
19720059817
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sharmahd, J. N.
(General Dynamics Corp. Convair Aerospace Div., San Diego, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
SAWE PAPER 943
Meeting Information
Meeting: Society of Aeronautical Weight Engineers, Annual Conference
Location: Atlanta, GA
Start Date: May 22, 1972
End Date: May 25, 1972
Sponsors: Society of Aeronautical Weight Engineers
Accession Number
72A43483
Funding Number(s)
CONTRACT_GRANT: NAS9-6796
CONTRACT_GRANT: NAS8-25021
CONTRACT_GRANT: NAS8-27539
Distribution Limits
Public
Copyright
Other

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